[lzlz]

Hi all,

Currently I need to model the 3D wing for lift and drag coefficient calculations. I need some 3D wind tunnel experimental data for the CFD validation so that I can feel more comfortable about my simulation data. Where could I find these 3D experimental data?

thanks!!!

[agd]

Try googling "ONERA M6"

[fluid23]

As agd suggests, ONERA M6 is a good option. Here are some others that I have used in the past as well...

Weber, J. and Brebner, G.G., ‘Low Speed Tests on 45-deg Swept-Back Wings. Part 1: Pressure Measurements on Wings of Aspect Ratio 5,’ Aeronautical Research Council, RM-2882, London, England, UK, ©1958.

Hall, I.M. and Rogers, E.W.E, ‘Experiments with a Tapered Sweptback Wing of Warren 12 Planform at Mach Numbers between 0.6 and 1.6,’ Aeronautical Research Council, RM-3271, London, England, UK, ©1962

Kolbe. C.D. and Boltz, F.W., ‘The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45

° Sweepback, Aspect Ratio of 3, and a Taper Ratio of 0.5,’ NACA RM-451G31, National Advisory Committee for Aeronautics, ©1951.



Graham, R.R., ‘Low-Speed Characteristics of a 45° Sweptback Wing of Aspect Ratio 8 from Pressure Distribution and Force Tests at Reynolds Numbers from 1,500,000 to 4,800,000,’NACA RM-L51H13, National Advisory Committee for Aeronautics, ©1951.

McAlister, K.W. and Takahasi, R.K., ‘NACA 0015 Wing Pressure and Trailing Vortex
Mesurements,’ NASA TP 3151, National Aeronautics and Space Administration,. Washington, D.C., ©1991.

Jacobs, W., ‘Pressure-Distribution Measurements on Unyawed Swept-Back Wings,’ NACA TM 1164, National Advisory Committee for Aeronautics, Washington, D.C., ©1947.

Johnson, H.S. and Hagerman, J.R., ‘Wind-Tunnel Investigation at Low Speed of An Unswept Untapered Semispan Wing of Aspect Ratio 3.13 Equiped with Various 25-Percent-Chord Plain Flaps,’ NACA TN 2080, National Advisory Committee for Aeronautics, Washington, D.C., ©1950.

[lzlz]

Originally Posted by agd

Try googling "ONERA M6"

thank u very much！

[lzlz]

Originally Posted by MBdonCFD

As agd suggests, ONERA M6 is a good option. Here are some others that I have used in the past as well...

Weber, J. and Brebner, G.G., ‘Low Speed Tests on 45-deg Swept-Back Wings. Part 1: Pressure Measurements on Wings of Aspect Ratio 5,’ Aeronautical Research Council, RM-2882, London, England, UK, ©1958.

Hall, I.M. and Rogers, E.W.E, ‘Experiments with a Tapered Sweptback Wing of Warren 12 Planform at Mach Numbers between 0.6 and 1.6,’ Aeronautical Research Council, RM-3271, London, England, UK, ©1962

Kolbe. C.D. and Boltz, F.W., ‘The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45

° Sweepback, Aspect Ratio of 3, and a Taper Ratio of 0.5,’ NACA RM-451G31, National Advisory Committee for Aeronautics, ©1951.



Graham, R.R., ‘Low-Speed Characteristics of a 45° Sweptback Wing of Aspect Ratio 8 from Pressure Distribution and Force Tests at Reynolds Numbers from 1,500,000 to 4,800,000,’NACA RM-L51H13, National Advisory Committee for Aeronautics, ©1951.

McAlister, K.W. and Takahasi, R.K., ‘NACA 0015 Wing Pressure and Trailing Vortex
Mesurements,’ NASA TP 3151, National Aeronautics and Space Administration,. Washington, D.C., ©1991.

Jacobs, W., ‘Pressure-Distribution Measurements on Unyawed Swept-Back Wings,’ NACA TM 1164, National Advisory Committee for Aeronautics, Washington, D.C., ©1947.

Johnson, H.S. and Hagerman, J.R., ‘Wind-Tunnel Investigation at Low Speed of An Unswept Untapered Semispan Wing of Aspect Ratio 3.13 Equiped with Various 25-Percent-Chord Plain Flaps,’ NACA TN 2080, National Advisory Committee for Aeronautics, Washington, D.C., ©1950.

Thank you very much for your answer. It's very helpful!